538106: BLADE,COMPRESSOR,AIRCRAFT GAS TU.
BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include material: TITANIUM ALLOY BLADE, design_type: COMPRESSOR, overall_width: 1.095 INCHES NOMINAL IN, overall_length: 3.472 INCHES NOMINAL IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE, material_thickness: 0.293 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 5340-00-884-9990, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | TITANIUM ALLOY BLADE |
| design_type | COMPRESSOR |
| overall_width | 1.095 INCHES NOMINAL IN |
| overall_length | 3.472 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| material_thickness | 0.293 INCHES NOMINAL IN |
| end_item_identification | TF30 ACFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | PWA1202 ASSN STD SINGLE MATERIAL RESPONSE BLADE |
| NSN | 5340-00-884-9990 |
| OVERALL HEIGHT | 0.1500 INCHES MINIMUM AND 0.1700 INCHES MAXIMUM IN |
| FSC APPLICATION DATA | CONTROL,PROPELLER |
| FIRST STEP DIAMETER | 0.4900 INCHES MINIMUM AND 0.5100 INCHES MAXIMUM IN |
| MATERIAL HARDNESS RATING | 70.0 ROCKWELL B MINIMUM AND 100.0 ROCKWELL B MAXIMUM |
| END DIAMETER | 0.3020 INCHES MINIMUM AND 0.3220 INCHES MAXIMUM IN |
| DISTANCE FROM END TO FIRST STEP | 0.0700 INCHES MINIMUM AND 0.0900 INCHES MAXIMUM IN |
| DESIGN TYPE | SOLID |
| SPECIAL FEATURES | SEAT BODY 1.024 IN. LG X 0.380 IN. WD X 0.160 IN. THK,RING CONCENTRIC TO END DIA GROUND ON 0.620/0.626 IN. DIA TO 0.080 IN. DEPTH,ONE HOLE 0.186/0.192 IN. DIA DRILLED THRU SEAT 0.540 IN. FROM CTR OF END DIA;NOT CASEHARDENED;MATL-STEEL AMS 5513 IN |
| MATERIAL | STEEL |
No substitute or cross-reference records for this part.